Works matching DE "FUSELAGE (Airplanes)"
Results: 167
Reduced-order modelling of non-linear, transient aerodynamics of the HIRENASD wing.
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- Aeronautical Journal, 2016, v. 120, n. 1226, p. 601, doi. 10.1017/aer.2016.12
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Modelling the aeroelastic response and flight dynamics of a hingeless rotor helicopter including the effects of rotor-fuselage aerodynamic interaction.
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- Aeronautical Journal, 2015, v. 119, n. 1214, p. 433, doi. 10.1017/S0001924000010563
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A fast procedure for the design of composite stiffened panels.
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- Aeronautical Journal, 2015, v. 119, n. 1212, p. 185, doi. 10.1017/S0001924000010332
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Flow over a glider canopy.
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- Aeronautical Journal, 2014, v. 118, n. 1204, p. 669, doi. 10.1017/S0001924000009428
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An analysis approach toward FAA certification for damage tolerance of aircraft components.
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- Aeronautical Journal, 2014, v. 118, n. 1200, p. 181, doi. 10.1017/S0001924000009064
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Efficient optimisation of large aircraft fuselage structures.
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- Aeronautical Journal, 2014, v. 118, n. 1199, p. 31, doi. 10.1017/S0001924000008915
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The use of topology optimisation in the conceptual design of next generation lattice composite aircraft fuselage structures.
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- Aeronautical Journal, 2013, v. 117, n. 1197, p. 1139, doi. 10.1017/S0001924000008745
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Evolving fuselage designs by incorporating SHM technologies.
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- Aeronautical Journal, 2011, v. 115, n. 1174, p. 749, doi. 10.1017/S0001924000006497
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On the generation of a helicopter aerodynamic database.
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- Aeronautical Journal, 2011, v. 115, n. 1164, p. 103, doi. 10.1017/S0001924000005492
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Computational aeroelastic studies of a generic hypersonic vehicle.
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- Aeronautical Journal, 2009, v. 113, n. 1150, p. 763, doi. 10.1017/S0001924000003420
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Aircraft cost modelling using the genetic causal technique within a systems engineering approach.
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- Aeronautical Journal, 2007, v. 111, n. 1121, p. 409, doi. 10.1017/S000192400000467X
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An integrated modeling method of unified tolerance representation for mechanical product.
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- International Journal of Advanced Manufacturing Technology, 2010, v. 46, n. 1-4, p. 217, doi. 10.1007/s00170-009-2062-3
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- Article
Spring-back characteristics of fiber metal laminate (GLARE) in brake forming process.
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- International Journal of Advanced Manufacturing Technology, 2007, v. 32, n. 5/6, p. 445, doi. 10.1007/s00170-005-0355-8
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Integrated layout and topology optimization design of multi-frame and multi-component fuselage structure systems.
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- Structural & Multidisciplinary Optimization, 2017, v. 56, n. 1, p. 21, doi. 10.1007/s00158-016-1645-5
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Numerical and experimental study on temperature and springback control of U-shape titanium extrusion hot stretch bending.
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- International Journal of Lightweight Materials & Manufacture, 2022, v. 5, n. 4, p. 453, doi. 10.1016/j.ijlmm.2022.05.007
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novel learning algorithm to estimate the optimum fuselage drag coefficient.
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- Sakarya University Journal of Science (SAUJS) / Sakarya Üniversitesi Fen Bilimleri Enstitüsü Dergisi, 2017, v. 21, n. 1, p. 63, doi. 10.16984/saufenbilder.59146
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Fundamental Design Optimization of an Innovative Supersonic Transport Configuration and Its Design Knowledge Extraction.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2016, v. 59, n. 6, p. 340, doi. 10.2322/tjsass.59.340
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Uncertain parameter numerical model updating according to variable modal test data in application of large composite fuselage panel.
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- Shock & Vibration, 2010, v. 17, n. 4/5, p. 445, doi. 10.1155/2010/507676
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Hybrid secondary suspension systems.
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- Shock & Vibration, 2009, v. 16, n. 5, p. 467, doi. 10.1155/2009/624170
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Fiber placement system produces one-piece composite fuselage.
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- Advanced Materials & Processes, 2006, v. 164, n. 3, p. 11
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Composite fuselage section completed for Boeing 7E7.
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- Advanced Materials & Processes, 2005, v. 163, n. 3, p. 66
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Fatigue and impact testing of composites.
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- Advanced Materials & Processes, 2002, v. 160, n. 10, p. 75
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Lightning strikes.
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- Advanced Materials & Processes, 2000, v. 158, n. 3, p. 71
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Materials Progress: Forming/Processing.
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- Advanced Materials & Processes, 1999, v. 156, n. 2, p. 16
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Materials progress: Welding/joining.
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- Advanced Materials & Processes, 1997, v. 152, n. 2, p. 14
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- Article
Analytical Determination of Residual Strength and Linkup Strength for Flat Panels, with Multiple Site Damage.
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- Arabian Journal for Science & Engineering (Springer Science & Business Media B.V. ), 2014, v. 39, n. 3, p. 2271, doi. 10.1007/s13369-013-0763-2
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A new NDT development using high-speed robots.
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- Insight: Non-Destructive Testing & Condition Monitoring, 2014, v. 56, n. 4, p. 178
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- Article
Towards a business enterprise strategy to support the integration of proactive aerospace maintenance technologies.
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- Insight: Non-Destructive Testing & Condition Monitoring, 2011, v. 53, n. 9, p. 502, doi. 10.1784/insi.2011.53.9.502
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Trend analysis of acousto-ultrasonic signals for integrity evaluation of metallic aerostructures.
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- Insight: Non-Destructive Testing & Condition Monitoring, 2010, v. 52, n. 3, p. 124, doi. 10.1784/insi.2010.52.3.124
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History Mystery.
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- Air Power History, 2009, v. 56, n. 3, p. 72
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Modelling framework for flight dynamics of flexible aircraft.
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- Aviation (1648-7788), 2016, v. 20, n. 4, p. 173, doi. 10.3846/16487788.2016.1264719
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FUSELAGE TEST OF A SMALL AIRCRAFT ACCORDING TO CS-23 REQUIREMENTS.
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- Aviation (1648-7788), 2009, v. 13, n. 1, p. 26, doi. 10.3846/1648-7788.2009.13.26-33
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OPTIMIZATION OF SPAR MASS AND FUSELAGE LOCATION TO DECREASE LOSS OF AIRPLANE LIFT FORCE.
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- Aviation (1648-7788), 2007, v. 11, n. 3, p. 21, doi. 10.3846/16487788.2007.9635965
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Crack growth in cylindrical aluminum shells with inner reinforcing foam layer.
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- International Journal of Fracture, 2007, v. 144, n. 3, p. 159, doi. 10.1007/s10704-007-9093-2
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Structural response of an aircraft fuselage to hydraulic system - A wave and mobility approach.
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- Noise Control Engineering Journal, 2013, v. 61, n. 1, p. 87, doi. 10.3397/1/1.3761009
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Four-pole modelling of vibration isolators: Application to SEA of aircraft double-wall panels subjected to mechanical excitation.
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- Noise Control Engineering Journal, 2012, v. 60, n. 2, p. 158, doi. 10.3397/1.3688316
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Greener Aviation Take-off (Delayed): Analysing Environmental Transitions with the Multi-Level Perspective.
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- Science & Technology Studies, 2015, v. 28, n. 1, p. 28, doi. 10.23987/sts.55356
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Modelling and Analysis of Vibrations in a UAV Helicopter with a Vision System.
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- International Journal of Advanced Robotic Systems, 2012, v. 9, n. 11, p. 1, doi. 10.5772/52761
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Numerical Simulation of the Four Roll Bending Process.
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- Materials & Manufacturing Processes, 2012, v. 27, n. 4, p. 370, doi. 10.1080/10426914.2011.560228
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Ultra-lightweight dual-polarized X-band array antenna for airborne weather radar applications.
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- Microwave & Optical Technology Letters, 2009, v. 51, n. 5, p. 1324, doi. 10.1002/mop.24323
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A crack propagation study on T-joints of AA6013-T4 aluminum alloy welded by an Yb:fiber laser.
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- International Journal of Advanced Manufacturing Technology, 2017, v. 92, n. 5-8, p. 2831, doi. 10.1007/s00170-017-0377-z
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Determining the minimum clamping force by cutting force simulation in aerospace fuselage pocket machining.
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- International Journal of Advanced Manufacturing Technology, 2015, v. 80, n. 9-12, p. 1751, doi. 10.1007/s00170-015-7104-4
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Study on analysis and prediction of riveting assembly variation of aircraft fuselage panel.
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- International Journal of Advanced Manufacturing Technology, 2014, v. 75, n. 5-8, p. 991, doi. 10.1007/s00170-014-6113-z
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Pesticide illness among flight attendants due to aircraft disinsectionInstitution where the work was performed: California Department of Health, Services, Occupational Health Branch, 850 Marina Bay Parkway, Building P, 3rd Floor, Richmond, CA 94804 (510) 620‐5757 Fax (510) 620‐5743.
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- American Journal of Industrial Medicine, 2007, v. 50, n. 5, p. 345, doi. 10.1002/ajim.20452
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Sampling of Chemical Constituents in Electrically Active Convective Systems: Results and Cautions.
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- Journal of Atmospheric Chemistry, 2006, v. 54, n. 1, p. 1, doi. 10.1007/s10874-005-9007-5
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- Article
Amplitude-Sensitive Single-Pumper Hydraulic Engine Mount Design without a Decoupler.
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- Applied Sciences (2076-3417), 2024, v. 14, n. 6, p. 2568, doi. 10.3390/app14062568
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Enhanced Efficiency and Reduced Side Lobe Level Convex Conformal Reflectarray.
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- Applied Sciences (2076-3417), 2021, v. 11, n. 21, p. 9893, doi. 10.3390/app11219893
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Buckling Test of Composite Cylindrical Shells with Large Radius Thickness Ratio.
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- Applied Sciences (2076-3417), 2021, v. 11, n. 2, p. 854, doi. 10.3390/app11020854
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Experimental and Numerical Study of Airflows in a Full-Scale Room.
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- ASHRAE Transactions, 2009, v. 115, n. 2, p. 867
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Influence of the Design Parameters of a Fuel Thermal Management System on Its Thermal Endurance.
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- Energies (19961073), 2018, v. 11, n. 7, p. 1677, doi. 10.3390/en11071677
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